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JP2013511643A - Aircraft engine module handling equipment - Google Patents

Aircraft engine module handling equipment Download PDF

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Publication number
JP2013511643A
JP2013511643A JP2012539344A JP2012539344A JP2013511643A JP 2013511643 A JP2013511643 A JP 2013511643A JP 2012539344 A JP2012539344 A JP 2012539344A JP 2012539344 A JP2012539344 A JP 2012539344A JP 2013511643 A JP2013511643 A JP 2013511643A
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module
tool
carriage
aircraft engine
engine module
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JP2012539344A
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JP5701310B2 (en
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ブーランジエ，パスカル
ダビド，ダニエル
エアリス，トーマ・ジユリアン・ロラン
マルシヤン，ジヤツク
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Safran Aircraft Engines SAS
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SNECMA SAS
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    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
    • B64F5/00—Designing, manufacturing, assembling, cleaning, maintaining or repairing aircraft, not otherwise provided for; Handling, transporting, testing or inspecting aircraft components, not otherwise provided for
    • B64F5/50—Handling or transporting aircraft components
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B66—HOISTING; LIFTING; HAULING
    • B66F—HOISTING, LIFTING, HAULING OR PUSHING, NOT OTHERWISE PROVIDED FOR, e.g. DEVICES WHICH APPLY A LIFTING OR PUSHING FORCE DIRECTLY TO THE SURFACE OF A LOAD
    • B66F7/00—Lifting frames, e.g. for lifting vehicles; Platform lifts
    • B66F7/06—Lifting frames, e.g. for lifting vehicles; Platform lifts with platforms supported by levers for vertical movement
    • B66F7/0625—Lifting frames, e.g. for lifting vehicles; Platform lifts with platforms supported by levers for vertical movement with wheels for moving around the floor
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B66—HOISTING; LIFTING; HAULING
    • B66F—HOISTING, LIFTING, HAULING OR PUSHING, NOT OTHERWISE PROVIDED FOR, e.g. DEVICES WHICH APPLY A LIFTING OR PUSHING FORCE DIRECTLY TO THE SURFACE OF A LOAD
    • B66F7/00—Lifting frames, e.g. for lifting vehicles; Platform lifts
    • B66F7/06—Lifting frames, e.g. for lifting vehicles; Platform lifts with platforms supported by levers for vertical movement
    • B66F7/065—Scissor linkages, i.e. X-configuration
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B66—HOISTING; LIFTING; HAULING
    • B66F—HOISTING, LIFTING, HAULING OR PUSHING, NOT OTHERWISE PROVIDED FOR, e.g. DEVICES WHICH APPLY A LIFTING OR PUSHING FORCE DIRECTLY TO THE SURFACE OF A LOAD
    • B66F9/00—Devices for lifting or lowering bulky or heavy goods for loading or unloading purposes
    • B66F9/06—Devices for lifting or lowering bulky or heavy goods for loading or unloading purposes movable, with their loads, on wheels or the like, e.g. fork-lift trucks

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  • Engineering & Computer Science (AREA)
  • Structural Engineering (AREA)
  • Transportation (AREA)
  • Life Sciences & Earth Sciences (AREA)
  • Geology (AREA)
  • Mechanical Engineering (AREA)
  • Civil Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Manufacturing & Machinery (AREA)
  • Automatic Assembly (AREA)
  • Handcart (AREA)
  • Testing Of Engines (AREA)
  • Packaging Of Machine Parts And Wound Products (AREA)

Abstract

このモジュールハンドリング装置（１）は、特に、台車（２）と、台車の上部の枢動部（５）と、モジュール支持ツール（１２）と、枢動部（５）にツールを取り付けるための追加の取り付け手段（１９）とを含み、モジュール（１）がクレート状態で組立工場に到着した時に見られる最初の垂直位置からエンジンの別のモジュールと組み合わせるのに適した水平位置になるように回転されることができる。  This module handling device (1) is in particular an additional for attaching the tool to the carriage (2), the pivot part (5) at the top of the carriage, the module support tool (12) and the pivot part (5) Mounting means (19) and rotated from a first vertical position seen when the module (1) arrives at the assembly plant in a crate to a horizontal position suitable for combination with another module of the engine. Can.

Description

本発明は、航空機エンジンのハンドリング装置に関する。   The present invention relates to an aircraft engine handling apparatus.

航空機エンジンは、最初は別個のモジュールに製造され、その後に互いに組み合わせられる。製造されたモジュールは、組立場所まで運ばれて、調整を経て、隣接するモジュールとドッキングされる位置に正確に移動される。この移動は、基本的には、手作業で行われるが、モジュールを持ち上げるホイストやモジュールを移動させる台車のような設備が利用できる。   Aircraft engines are initially manufactured in separate modules and then combined with each other. The manufactured module is transported to an assembly site, adjusted, and accurately moved to a position where it is docked with an adjacent module. This movement is basically performed manually, but facilities such as a hoist for lifting the module and a carriage for moving the module can be used.

独国特許出願公開第３４２７０４２号明細書German Patent Application Publication No. 3427042 米国特許第１４８１５０３号明細書US Pat. No. 1,481,503 米国特許第１６００８３５号明細書US Pat. No. 1,600,845 米国特許出願公開第２００９／０２０９３４号明細書US Patent Application Publication No. 2009/020934 米国特許第５８６３０３４号明細書US Pat. No. 5,863,034

航空機エンジンモジュールは、かさ張る重い部品であるが壊れやすいので、この手作業は、時間がかかる上に難しい。特に問題となるのは、これらのモジュールは、通常、回転軸を水平にして組み立てられるが、配送時は、平らな端部の表面に載るように、また配送時の安定性を良くするために、クレート内では回転軸が垂直に配置されることが多いので、クレートから取り出す時に、通常は、台車に配置する前にひっくり返さなければならないが、この作業は難しく、かなり注意が必要であるということである。モジュールを台車に配置するのも難しい作業であり、モジュールを安定した形で十分な面積で台車に載せることができるように、「ラグ」と呼ばれる特別なブラケットをモジュールに付けなければならない。そうしなければ、モジュールは、一般に、円錐形または一様でない回転形状を有するので、安定した形で台車に載せることができない。さらに、モジュールを補強すると同時に、モジュールが他のモジュールと組み合わされる前にロータとステータ間の運動を防ぐために、モジュールの端部で組み立てられる「ストロングバック」と呼ばれるツールを使用する必要があることを付け加えなければならない。   Aircraft engine modules are bulky and heavy parts but are fragile, so this manual operation is time consuming and difficult. Of particular concern is that these modules are usually assembled with the axis of rotation level, but during delivery, they should rest on the flat end surface and improve stability during delivery. In the crate, the axis of rotation is often arranged vertically, so when removing it from the crate, it usually has to be turned over before placing it on the carriage, but this is difficult and requires considerable care It is. Placing the module on the trolley is also a difficult task, and a special bracket called a “lag” must be attached to the module so that the module can be placed on the trolley in a stable and sufficient area. Otherwise, the module generally has a conical shape or a non-uniform rotational shape, so it cannot be placed on the carriage in a stable manner. In addition, it is necessary to use a tool called “strong back” assembled at the end of the module to reinforce the module and prevent movement between the rotor and stator before the module is combined with other modules. It must be added.

本発明は、上述の不利点を避け、最適な作業条件下で、より迅速に、手作業がはるかに少なくなり事前注意が少なくて済むように、モジュールと隣接モジュールとの組立の準備を行うことができる航空機エンジンモジュールのハンドリング装置に関する。   The present invention avoids the above disadvantages and prepares the assembly of modules and adjacent modules so that under optimum working conditions, more quickly, with much less manual labor and less precautions. The present invention relates to an aircraft engine module handling apparatus that can perform the above-described operations.

独国特許出願公開第３４２７０４２号明細書には、可動台車にモジュールを取り付ける手段とモジュールの位置を調節する手段とが取り付けられた航空機エンジンハンドリング装置が記載されているが、本発明の他の特徴を想起するものではなく、特にモジュールの端部に固定されたツールで取り付けを行うものでもなく、また完全にモジュールを倒すことができるものでもない。他の台車または支持装置が、米国特許第１４８１５０３号明細書、米国特許第１６００８３５号明細書、米国特許出願公開第２００９／０２０９３４号明細書、米国登録特許第５８６３０３４号明細書に記載されている。   German Patent Publication No. 3427042 describes an aircraft engine handling device having means for attaching the module to the movable carriage and means for adjusting the position of the module. Is not intended to be mounted, especially with a tool fixed to the end of the module, nor is it possible to completely collapse the module. Other trolleys or support devices are described in US Pat. No. 1,481,503, US Pat. No. 1,600,985, US Patent Application Publication No. 2009/020934, US Pat. No. 5,863,034.

本発明は、一般的には、航空機エンジンモジュールハンドリング装置に関し、可動台車と、モジュールの端部に位置決めされたツールとを含み、ツールがマウントとモジュールの取り付け装置とを含む航空機エンジンモジュールハンドリング装置であって、台車は、モジュール支持フレームに配設され水平軸を中心として枢動する上部補強構造体を含み、上部補強構造体およびツールは、モジュールの軸が水平軸と交差する位置でモジュールを台車に固定するための追加の装置を含むことを特徴とする航空機エンジンモジュールハンドリング装置に関する。   The present invention relates generally to aircraft engine module handling devices, and includes an aircraft engine module handling device that includes a movable carriage and a tool positioned at an end of the module, the tool including a mount and a module mounting device. The carriage includes an upper reinforcing structure disposed on the module support frame and pivoting about a horizontal axis, and the upper reinforcing structure and the tool move the module at a position where the axis of the module intersects the horizontal axis. The present invention relates to an aircraft engine module handling device characterized in that it includes an additional device for fixing to the aircraft engine module.

このようにして、エンジンモジュールは、有利には本発明に適切な「ストロングバック」であるツールを介して台車に固定される、つまり、モジュールは、直接または「ラグ」を介して台車に載せられることはないので、衝撃または過度の接触圧力によって損傷するリスクを低減することができる。また、モジュールは回転軸が垂直である搬送形態から回転軸が水平である組立形態に変化する必要があるが、モジュールを倒すのは台車によってのみ行われ、衝突を防ぐために、またはモジュールによる位置合わせを調節するために何の努力も特別な注意も払う必要がない。   In this way, the engine module is advantageously fixed to the carriage via a tool that is “strong back” suitable for the present invention, ie the module is mounted directly or via a “lug” on the carriage. Nevertheless, the risk of damage by impact or excessive contact pressure can be reduced. In addition, the module needs to be changed from a transport configuration in which the rotation axis is vertical to an assembly configuration in which the rotation axis is horizontal. However, the module is only tilted by the carriage, and in order to prevent a collision or alignment by the module There is no need to make any effort or special attention to adjust the.

組立の重要なポイントは、モジュールが組み合わされる時にモジュールの高さを調節するために、フレームを持ち上げることである。これは、台車から独立可能な装置によって行われ、この装置は、組立が行われ得る位置に固定テーブルを含む。台車はテーブルの上に持ち上げられ、テーブルが台車を所望の高さまで上昇させるが、モジュールは台車にしっかりと取り付けられた状態のままである。   An important point of assembly is to lift the frame to adjust the height of the module when the modules are assembled. This is done by a device that is independent of the carriage, which includes a fixed table in a position where assembly can take place. The trolley is lifted onto the table and the table raises the trolley to the desired height, but the module remains securely attached to the trolley.

組立は、モジュールを台車から取り外して、ホイストによってモジュールを持ち上げて行われることができる。ハンドリング装置は、リフトアームを付けることによって完成される。リフトアームは、モンジュールの一端から他端に延在し、例えば、一端がモジュールに取り付けられ、他端がツールに取り付けられ、リフトアームがモジュールの重心位置で持ち上げられるようにする取り付け手段が装着されるので、モジュールが倒れる危険性がなくなる。   Assembly can be done by removing the module from the carriage and lifting the module by a hoist. The handling device is completed by attaching a lift arm. The lift arm extends from one end of the monjoule to the other end, for example, one end is attached to the module, the other end is attached to the tool, and mounting means is attached to allow the lift arm to be lifted at the center of gravity of the module This eliminates the risk of the module falling over.

図面を使用して、本発明をより詳細に説明する。   The invention is explained in more detail using the drawings.

台車に取り付けられたモジュールを示す図である。It is a figure which shows the module attached to the trolley | bogie. 台車に取り付けられたモジュールを倒した後の様子を示す図である。It is a figure which shows the mode after defeating the module attached to the trolley | bogie. 台車に取り付けられたモジュールを倒した後の様子を示す図である。It is a figure which shows the mode after defeating the module attached to the trolley | bogie. 台車が使用される前の組立位置に到着した時のモジュールを示す図である。It is a figure which shows a module when it arrives at the assembly position before a trolley | bogie is used. 台車に設置される直前のモジュールを示す図である。It is a figure which shows the module just before installing in a trolley | bogie.

本発明の本実施形態に示される航空機エンジンモジュール１は、「コア」または高圧本体と呼ばれる。これは、圧縮機、高圧タービン、および燃焼室を含む主中間モジュールである。図１〜図３に示されるように、モジュール１は、台車２に取り付けられる。台車２は、フレーム３と、フレーム３に設置されるローラ４と、フレーム３から上に伸びてモジュール１を支持する補強構造体５とを含む。しかしながら、台車２は、リフト装置６によって地上から持ち上げられて支えられており、リフト装置６は、フレーム７と、特にフレーム７の位置に位置決めされて台車２のフレーム３が設置される上部テーブル８と、テーブル８と地上との間に位置する個々の中央で接続されたバー１０を有する機構９とを含み、機構９は、バー１０の接続角がジャッキ１１によって変更されると、このテーブルを持ち上げる働きをする。装置の別の要素は、カバー１の後部に取り付けられるカバーの形状のツール１２である。ツール１２は、本来は、当分野で知られている「ストロングバック」であり、主に、モジュール１の後部を覆うプレートでできたマウント１３であって、図示されていない装置によってモジュール１がネジ留めまたは別の方法で取り付けられ、モジュール１を補強してモジュール１を保護することができるマウント１３と、図示されていないが既知であるように、マウント１３によって支持されてモジュール１のロータとステータ間の摺り運動および回転運動を防ぐ手段とを含む。しかし、ツール１２は、知られているストロングバックの改良されたものである。つまり、ツール１２は、リフトアーム１５が取り付けられる上部突出部１４を含み、リフトアーム１５の他端部１６はモジュール１の前面に取り付けられ、リフトアーム１５は中心に取り付けリング１８を有する。リフトアームの取り付けは、取り外し可能なピン３７を突出部１４に差し込んで、モジュール１の前面のフランジ１７にネジ留めすることで行われる。   The aircraft engine module 1 shown in this embodiment of the present invention is referred to as a “core” or high pressure body. This is the main intermediate module including the compressor, high pressure turbine, and combustion chamber. As shown in FIGS. 1 to 3, the module 1 is attached to a carriage 2. The carriage 2 includes a frame 3, a roller 4 installed on the frame 3, and a reinforcing structure 5 that extends upward from the frame 3 and supports the module 1. However, the carriage 2 is supported by being lifted from the ground by the lift device 6. The lift device 6 is positioned at the position of the frame 7, particularly the frame 7, and the upper table 8 on which the frame 3 of the carriage 2 is installed. And a mechanism 9 having individual centrally connected bars 10 located between the table 8 and the ground, which mechanism 9 can be used when the connection angle of the bar 10 is changed by the jack 11. It works to lift. Another element of the device is a tool 12 in the form of a cover that is attached to the rear of the cover 1. The tool 12 is essentially a “strong back” known in the art, and is mainly a mount 13 made of a plate that covers the rear of the module 1, and the module 1 is screwed by a device not shown. A mount 13 that can be fastened or otherwise attached to reinforce the module 1 to protect the module 1 and, as is known, not shown, supported by the mount 13 and the rotor and stator of the module 1 And means for preventing intercalation and rotational movement. However, the tool 12 is an improvement of the known strongback. That is, the tool 12 includes an upper protrusion 14 to which the lift arm 15 is attached, the other end 16 of the lift arm 15 is attached to the front surface of the module 1, and the lift arm 15 has a mounting ring 18 at the center. The lift arm is attached by inserting a detachable pin 37 into the protrusion 14 and screwing it onto the flange 17 on the front surface of the module 1.

装置の他の要素は、ツール１２と台車２との追加の取り付け手段１９であり、取り付け手段１９は、ツール１２の側で真っ直ぐに伸びる突出部２０と、突出部２０の端部にあるブロック状のスキッド２１と、補強構造体５の上部のブラケット２６によって調整される張り出し縁部２３によって画定される溝２２と、溝２２の底部にある止め具２４と、溝２２のスキッド２１とブラケット２６とを留めるネジ２５とを含む。ブラケット２６には、水平軸を有するピボット２７が取り付けられており、補強構造体５に組み合わせられ、モータ２８によって駆動されて、補強構造体５がこの軸を中心として回転できるようにする。   The other element of the device is an additional attachment means 19 between the tool 12 and the carriage 2, the attachment means 19 being a protrusion 20 extending straight on the side of the tool 12 and a block-like shape at the end of the protrusion 20. The skid 21, the groove 22 defined by the overhang edge 23 adjusted by the bracket 26 at the top of the reinforcing structure 5, the stop 24 at the bottom of the groove 22, the skid 21 and the bracket 26 in the groove 22, And a screw 25 for fastening. A pivot 27 having a horizontal axis is attached to the bracket 26 and is combined with the reinforcing structure 5 and driven by a motor 28 so that the reinforcing structure 5 can be rotated about this axis.

以下に説明する装置を使用したモジュール１のハンドリング方法について説明する。図４は、最初の形態のモジュール１を示しており、クレート２９内に収容され、回転軸は垂直であり、モジュール１の後部が上方に向けられている。第１のステップは、クレート２９からカバー３０を取り外し、モジュール１が動かないように設計された構造体３１を取り外すステップである。このステップが行われる時は、モジュール１はまだクレート３０の基部３２に置かれているが解放された状態であり、モジュール１にツール１２が取り付けられ、その後、ツール１２はホイスト３３から懸架される。ホイスト３３は、突出部２０と、ツール１２の反対側から突出するハンドル３４（図２に示される）とに取り付けられる。そして、図５の状態になる。ホイスト３３は、ツール１２とモジュール１とを取り外すことで持ち上げられ、その後、同じように保護カバーを有するツールがモジュール１の前面（ツール１２から反対側端部）にも配置され、その後、モジュール１は台車２に設置される。前面のツール（図示せず）は、知られているタイプの「ストロングバック」ツールであるが、より軽量であり、本発明によって得られるハンドリングの安全性のために手作業で設置でき、このツールによってモジュール１に付与される力は小さくなる。台車２への設置は、スキッド２１を溝２２に案内し（スキッドは垂直に配向される）、モジュール１の先端部品を止め具２４の位置で止まるまで下げて、ネジ２５を留めることにより、図１の姿勢となり完成される。次のステップは、モジュール１を倒すことによって図３の状態になるように、モジュール１の軸と交差する軸でピボット２７を回転させることである。この場合、モジュール１の軸は水平になり、モジュール１の前面は台車の片側から突き出ている。リフトアーム１５が装置の上部に設置され、リフトアームが取り付けられる突出部１４は上方に向けられる。その後、台車２は、リフト装置６のテーブル８の上にくるまで移動されて、低い位置まで下げられてフレーム７に収容され、フレーム３の前方および後方に配置された旋回伸縮式の止め具３５が下ろされる。ジャッキ１１を操作することで、テーブル８は上昇されて、台車２およびモジュール１を持ち上げることができる。台車２の不測の落下は、止め具３５、およびテーブル８を四隅で囲むローラ４によって防がれる。ホイスト３３は、リフトアーム１５を使用してアームでモジュール１を取り上げ、組立手段１９が分離されると台車２からモジュール１を持ち上げて、モジュール１がエンジンの別のモジュール３６とドッキングされるまでモジュール１を移動させて、モジュール１は別のモジュール３６に組み合わせられる。リング１８はモジュール１の重心の上に位置決めされるので、モジュール１が倒れる危険性がなくなる。   A method for handling the module 1 using the apparatus described below will be described. FIG. 4 shows the first form of the module 1, which is housed in a crate 29, the axis of rotation is vertical and the rear of the module 1 is oriented upwards. The first step is to remove the cover 30 from the crate 29 and remove the structure 31 designed so that the module 1 does not move. When this step is performed, the module 1 is still in the base 32 of the crate 30 but released, the tool 12 is attached to the module 1 and then the tool 12 is suspended from the hoist 33. . The hoist 33 is attached to the protrusion 20 and a handle 34 (shown in FIG. 2) protruding from the opposite side of the tool 12. And it will be in the state of FIG. The hoist 33 is lifted by removing the tool 12 and the module 1, and then a tool having a protective cover is also placed on the front surface of the module 1 (the opposite end from the tool 12). Is installed on the carriage 2. The front tool (not shown) is a known type of “strong back” tool, but is lighter and can be manually installed for handling safety provided by the present invention. As a result, the force applied to the module 1 is reduced. Installation on the carriage 2 is achieved by guiding the skid 21 into the groove 22 (the skid is oriented vertically), lowering the tip part of the module 1 until it stops at the position of the stopper 24, and fastening the screw 25. Completed with 1 posture. The next step is to rotate the pivot 27 about an axis that intersects the axis of the module 1 so that the state of FIG. In this case, the axis of the module 1 is horizontal, and the front surface of the module 1 protrudes from one side of the carriage. A lift arm 15 is installed in the upper part of the apparatus, and the protrusion 14 to which the lift arm is attached is directed upward. Thereafter, the carriage 2 is moved until it is on the table 8 of the lift device 6, lowered to a low position, accommodated in the frame 7, and a swivel telescopic stopper 35 disposed in front and rear of the frame 3. Is lowered. By operating the jack 11, the table 8 is raised and the carriage 2 and the module 1 can be lifted. The accidental fall of the carriage 2 is prevented by the stopper 35 and the roller 4 surrounding the table 8 at the four corners. The hoist 33 picks up the module 1 with the arm using the lift arm 15 and lifts the module 1 from the carriage 2 when the assembly means 19 is separated, until the module 1 is docked with another module 36 of the engine. Module 1 is combined with another module 36 by moving one. Since the ring 18 is positioned on the center of gravity of the module 1, there is no risk of the module 1 falling over.

上述した操作のいくつかは、特に、モジュール１の回転、ホイスト３３の取り外し、テーブル８の持ち上げは異なる順序で行われれもよい。モジュール１の組立位置の近くに固定持ち上げ装置６が示されているが、これは必須ではなく、持ち上げ装置６は台車２に組み込まれてもよいことに留意されたい。   Some of the operations described above may be performed in a different order, in particular the rotation of the module 1, the removal of the hoist 33 and the lifting of the table 8. It should be noted that although a fixed lifting device 6 is shown near the assembly position of the module 1, this is not essential and the lifting device 6 may be integrated into the carriage 2.

Claims (5)

可動台車（２）とモジュール（１）の端部に位置決めされるツール（１２）とを含み、ツールはマウント（１３）とモジュールに取り付けるための装置とを含む、航空機エンジンモジュールハンドリング装置（１）であって、台車は、モジュール支持フレーム（３）上に設けられ水平軸を中心として枢動する（２７）上部補強構造体（５）を含み、上部補強構造体（５）およびツール（１２）は、モジュールの回転軸が水平軸と交差する位置でモジュールを台車に固定するための追加の装置（１９）を含むことを特徴とする、航空機エンジンモジュールハンドリング装置。   An aircraft engine module handling device (1) comprising a movable carriage (2) and a tool (12) positioned at the end of the module (1), the tool comprising a mount (13) and a device for attaching to the module The carriage includes an upper reinforcement structure (5) provided on the module support frame (3) and pivoting about a horizontal axis (27), the upper reinforcement structure (5) and the tool (12). An aircraft engine module handling device, characterized in that it includes an additional device (19) for fixing the module to the carriage at a position where the axis of rotation of the module intersects the horizontal axis. 追加の取り付け装置は、張り出し縁部（２３）によって画定される溝（２２）を含み、溝（２２）内を摺動しツール（１２）の突出部（２０）に取り付けられるスキッド（２１）が溝より外に延在し、さらに溝内のスキッドの止め具（２４）と溝内の止め具の位置でスキッドを固定する手段（２５）とを含むことを特徴とする、請求項１に記載の航空機エンジンモジュールハンドリング装置。   The additional attachment device includes a groove (22) defined by an overhang edge (23), and a skid (21) that slides within the groove (22) and is attached to the protrusion (20) of the tool (12). 2. A skid stop (24) extending out of the groove and further comprising means (25) for securing the skid at the position of the stop in the groove. Aircraft engine module handling equipment. フレーム（３）を持ち上げるための装置（６）を含むことを特徴とする、請求項１または２のいずれかに記載の航空機エンジンモジュールハンドリング装置。   3. An aircraft engine module handling device according to claim 1 or 2, characterized in that it comprises a device (6) for lifting the frame (3). フレームを持ち上げるための装置（６）は、台車から独立したテーブル（８）を含み、テーブル（８）上で台車は転がることができ、テーブル（８）と台車（２）との間に固定止め具（３５）があることを特徴とする、請求項３に記載の航空機エンジンモジュールハンドリング装置。   The device for lifting the frame (6) comprises a table (8) independent of the carriage, on which the carriage can roll and is fixed between the table (8) and the carriage (2). Aircraft engine module handling device according to claim 3, characterized in that there is a tool (35). 一端がツール（１２）に取り付けられ、反対端（１６）がツールの反対側のモジュールの位置（１７）に取り付けられることのできるリフトアーム（１５）を含むことを特徴とする、請求項１から４のうちいずれか１項に記載の航空機エンジンモジュールハンドリング装置。   2. The lift arm (15) according to claim 1, characterized in that it comprises a lift arm (15) with one end attached to the tool (12) and the opposite end (16) attached to the position (17) of the module opposite the tool. 5. The aircraft engine module handling device according to claim 1.
JP2012539344A 2009-11-20 2010-11-19 Aircraft engine module handling equipment Active JP5701310B2 (en)

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FR0958240A FR2952922B1 (en) 2009-11-20 2009-11-20 HANDLING ASSEMBLY FOR AN AIRCRAFT ENGINE MODULE
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PCT/EP2010/067858 WO2011061307A1 (en) 2009-11-20 2010-11-19 Assembly for handling an aircraft engine

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CN102666360A (en) 2012-09-12
BR112012011998B1 (en) 2020-08-11
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RU2544425C2 (en) 2015-03-20
RU2012124417A (en) 2013-12-27
EP2501642B1 (en) 2013-10-16
US9309008B2 (en) 2016-04-12
CA2781226A1 (en) 2011-05-26
CN102666360B (en) 2015-04-01
WO2011061307A1 (en) 2011-05-26
EP2501642A1 (en) 2012-09-26
US20120224944A1 (en) 2012-09-06
FR2952922B1 (en) 2012-05-25
JP5701310B2 (en) 2015-04-15
FR2952922A1 (en) 2011-05-27

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